Air-Spring Compensation in a Piston-Type Marine Vibrator

ABSTRACT

Embodiments relate to the restriction of gas flow in a piston-type marine vibrator to compensate for air-spring effects. An embodiment provides marine vibrator comprising: a containment housing; a piston plate; a fixture coupled to the containment housing; a mechanical spring element coupled to the piston plate and to the fixture; a driver coupled to the piston plate and to the fixture; and a variable gas flow restrictor disposed in an interior volume of the marine vibrator, wherein the marine vibrator has a resonance frequency selectable based at least in part on the variable gas flow restrictor.

CROSS-REFERENCE TO RELATED APPLICATIONS

The present application claims priority to U.S. Nonprovisionalapplication Ser. No. 14/284,847, filed on May 22, 2014, which claimspriority to U.S. Provisional Application No. 61/880,561, filed on Sep.20, 2013, the entire disclosure of which is incorporated herein byreference.

BACKGROUND

Embodiments relate generally to piston-type marine vibrators for marinegeophysical surveys. More particularly, embodiments relate to therestriction of gas flow in a piston-type marine vibrator to compensatefor air-spring effects.

Sound sources are generally devices that generate acoustic energy. Oneuse of sound sources is in marine seismic surveying in which the soundsources may be employed to generate acoustic energy that travelsdownwardly through water and into subsurface rock. After interactingwith the subsurface rock, for example, at boundaries between differentsubsurface layers, some of the acoustic energy may be reflected backtoward the water surface and detected by specialized sensors, in thewater, typically either on the water bottom or towed on one or morestreamers. The detected energy may be used to infer certain propertiesof the subsurface rock, such as structure, mineral composition and fluidcontent, thereby providing information useful in the recovery ofhydrocarbons.

Most of the sound sources employed today in marine seismic surveying areof the impulsive type, in which efforts are made to generate as muchenergy as possible during as short a time span as possible. The mostcommonly used of these impulsive-type sources are air guns thattypically utilize compressed air to generate a sound wave. Otherexamples of impulsive-type sources include explosives and weight-dropimpulse sources. Another type of sound source that can be used in marineseismic surveying includes marine vibrators, such as hydraulicallypowered sources, electro-mechanical vibrators, electrical marine seismicvibrators, and sources employing piezoelectric or magnetostrictivematerial. Marine vibrators typically generate vibrations through a rangeof frequencies in a pattern known as a “sweep” or “chirp.”

Prior sound sources for use in marine seismic surveying have typicallybeen designed for relatively high-frequency operation (e.g., above 10Hz). However, it is well known that as sound waves travel through waterand through subsurface geological structures, higher frequency soundwaves may be attenuated more rapidly than lower frequency sound waves,and consequently, lower frequency sound waves can be transmitted overlonger distances through water and geological structures than can higherfrequency sound waves. Thus, efforts have been undertaken to developsound sources that can operate at lower frequencies. Very low frequencysources (“VLFS”) have been developed that typically have at least oneresonance frequency of about 10 Hz or lower. VLFS's are typicallycharacterized by having a source size that is very small as compared toa wavelength of sound for the VLFS. The source size for a VLFS istypically much less than 1/10^(th) of a wavelength and more typically onthe order of 1/100^(th) of a wavelength. For example, a source with amaximum dimension of 3 meters operating at 5 Hz is 1/100^(th) of awavelength in size.

In order to achieve a given level of output in the water, a marinevibrator typically needs to undergo a change in volume. In order to workat depth while minimizing structural weight, the marine vibrator may bepressure balanced with external hydrostatic pressure. As the internalgas (e.g., air) in the marine vibrator increases in pressure, the bulkmodulus (or “stiffness”) of the internal gas also rises. Increasing thebulk modulus of the internal gas also increases the air-spring effectwithin the marine vibrator. As used herein, the term “air-spring” isdefined as an enclosed volume of gas (e.g., air) that may absorb shockor fluctuations of load due to the ability of the enclosed volume of gasto resist compression and decompression. Increasing the stiffness of thegas in the enclosed volume, increases the air-spring effect and thus theability of the enclosed volume of gas to resist compression anddecompression. This increase in the air-spring effect of the internalgas tends to be a function of the operating depth of the source.Further, the stiffness of the acoustic components of the marine vibratorand the internal gas are the primary determining factors in the marinevibrator's resonance frequency. Accordingly, the resonance frequencygenerated by the marine vibrator may undesirably increase when themarine vibrator is towed at depth, especially in marine vibrators wherethe interior volume of the marine vibrator may be pressure balanced withthe external hydrostatic pressure.

BRIEF DESCRIPTION OF THE DRAWINGS

These drawings illustrate certain aspects of some of the embodiments ofthe present invention and should not be used to limit or define theinvention.

FIG. 1 illustrates an example embodiment of a marine vibrator with avariable gas flow restrictor.

FIG. 2 illustrates the change in the air-spring effect as the pressureand volume of the internal gas is altered in accordance with exampleembodiments.

FIG. 3 illustrates the shift in resonance frequency due to theair-spring effect as the marine vibrator is being towed deeper inaccordance with example embodiments.

FIG. 4 illustrates simulated amplitude spectra showing the expectedeffect of compressed gas that generates an air-spring as the marinevibrator is being towed deeper in accordance with example embodiments.

FIG. 5 illustrates an example embodiment of a variable gas flowrestrictor for use with a marine vibrator.

FIG. 6 illustrates a partial cross-sectional view of an exampleembodiment of a marine vibrator.

FIG. 7 illustrates a cross-sectional view of the marine vibrator of FIG.6 taken along line 1-1.

FIG. 8 illustrates a cross-sectional view of the marine vibrator of FIG.6 taken along line 2-2.

FIG. 9 illustrates a cross-sectional view of an embodiment of a marinevibrator with an alternative embodiment of mechanical spring elementtaken along line 3-3 of FIG. 6.

FIG. 10 illustrates another example embodiment of the marine vibrator ofFIG. 6 with a variable gas flow restrictor in cross-section.

FIG. 11 is an example embodiment of a marine seismic survey system usinga marine vibrator.

DETAILED DESCRIPTION

It is to be understood that the present disclosure is not limited toparticular devices or methods, which may, of course, vary. It is also tobe understood that the terminology used herein is for the purpose ofdescribing particular embodiments only, and is not intended to belimiting. All numbers and ranges disclosed herein may vary by someamount. Whenever a numerical range with a lower limit and an upper limitis disclosed, any number and any included range falling within the rangeare specifically disclosed. Although individual embodiments arediscussed, the invention covers all combinations of all thoseembodiments. As used herein, the singular forms “a”, “an”, and “the”include singular and plural referents unless the content clearlydictates otherwise. Furthermore, the word “may” is used throughout thisapplication in a permissive sense (i.e., having the potential to, beingable to), not in a mandatory sense (i.e., must). The term “include,” andderivations thereof, mean “including, but not limited to.” The term“coupled” means directly or indirectly connected. If there is anyconflict in the usages of a word or term in this specification and oneor more patent or other documents that may be incorporated herein byreference, the definitions that are consistent with this specificationshould be adopted for the purposes of understanding this invention.

Embodiments relate generally to marine vibrators for marine geophysicalsurveys that incorporate one or more piston plates that may act on thesurrounding water to produce acoustic energy. In embodiments, the marinevibrators may further comprise one or more drivers coupled to the pistonplates to cause the piston plates to move back and forth. The marinevibrators may also include one or more springs coupled to the pistonplates and a fixture. The marine vibrators define an internal volume inwhich a gas may be disposed. The gas may be any gas or combination ofgases (e.g., air, oxygen, nitrogen, carbon dioxide, etc.) that isselected based on the expected operational requirements of the device.One of ordinary skill in the art with the benefit of this disclosureshould be able to select an appropriate gas or combination of gas foruse in the marine vibrator. In one or more embodiments, gas flow may berestricted in a marine vibrator to compensate for air-spring (also knownas “gas-spring”) effects. As discussed in more detail below, the gasflow in the marine vibrator may be restricted to make the air-springmore or less stiff to thereby adjust the first resonance frequency atdepth.

FIG. 1 illustrates an example embodiment of a marine vibrator 5 thatincludes a variable gas restrictor 10, for example, to restrict gas flowand, thus, compensate for air-spring effects. In the illustratedembodiment, marine vibrator 5 is a piston-type marine vibrator. Asillustrated, marine vibrator 5 may include piston plates 15. For thesake of simplicity, this generalized example embodiment provides ageneral embodiment of the shape and location of piston plates 15;furthermore some of the internal components of marine vibrator 5 areremoved so as to not completely or partially obscure the illustratedcomponents. By way of example, piston plates 15 and the containmenthousing (as best seen in FIGS. 6-8) may at least partially define aninternal volume in which a gas may be disposed, as such the gas disposedwithin marine vibrator 5 may comprise an internal gas pressure. In someembodiments, marine vibrator 5 may comprise a pressure-compensationsystem. The pressure-compensation system may be used, for example, toequalize the internal gas pressure of marine vibrator 5 with theexternal pressure. Pressure compensation may be used, for example, wheremarine vibrator 5 needs to be towed at depth to achieve a given level ofoutput. As the depth of marine vibrator 5 increases, the internal gaspressure may be increased to equalize pressure with the increasingexternal pressure. A gas (e.g., air) may be introduced into marinevibrator 5, for example, to increase the internal gas pressure.

As illustrated, marine vibrator 5 may further include one or moredrivers 20, which may be electro-dynamic drivers, for example. Drivers20 may be coupled to piston plates 15. As illustrated, marine vibrator 5may further include a fixture 25 capable of suspending drivers 20 withinmarine vibrator 5. In the illustrated embodiment, fixture 25 may be inthe form of a frame.

In the illustrated embodiment of FIG. 1, variable gas flow restrictor 10is disposed within the internal volume of marine vibrator 5. Asillustrated, variable gas flow restrictor 10 may be secured to fixture25. In example embodiments, variable gas flow restrictor 10 has asliding-plate structure that may be movable between a closed positionand an open position. In the closed or partially closed position,variable gas flow restrictor 10 may be used to restrict gas flow inmarine vibrator 5. In some embodiments, variable gas flow restrictor 10may completely seal off a portion of the internal volume of marinevibrator 5. Accordingly, the gas flow may be restricted when desired tomake the air-spring stiffer, which may be desired in some embodiments.By way of example, it may be desired to make the air-spring stiffer andthus increase the first resonance frequency at shallow depths. This typeof air-spring compensation may be performed, for example, when asubstantially constant resonance frequency is desired regardless ofdepth. Without air-spring compensation, the air-spring has a tendency tostiffen as marine vibrator 5 is lowered in the water, thereby causingthe first resonance frequency to vary with depth. However, presentembodiments may provide a resonance frequency for marine vibrator 5selected at least in part on variable gas flow restrictor 10 such thatmarine vibrator 5 may have a substantially constant resonance frequencyregardless of depth.

Those of ordinary skill in the art, with the benefit of this disclosure,should appreciate that an increase in the internal gas pressure of themarine vibrator 5 may also result in an increase of the bulk modulus orair-spring effect of the gas (e.g., air) in the marine vibrator 5. Amongother things, the resonance frequency of marine vibrator 5 is based onthe combination of the air-spring of the gas in marine vibrator 5 andthe spring constant of the mechanical spring (e.g., mechanical springelements 110 on FIG. 6-10). Thus, increasing the air-spring effect ofthe internal gas of marine vibrator 5 may also result in an increase inthe resonance frequency. As such, the resonance frequency of a marinevibrator 5 towed at depth may undesirably vary when towed at varyingdepths.

FIGS. 2 and 3 illustrate the effect of an air-spring on a marinevibrator 5 at various depths in accordance with example embodiments. InFIG. 2, the volume of the internal gas defined by marine vibrator 5 isrepresented by reference number 30. To illustrate the air-spring effect,the volume 30 of the internal gas is shown at ambient pressure at 35,under compression at 40, and under expansion at 45. Therefore, FIG. 2illustrates the relationship between pressure and volume in relation tothe air-spring effect. Thus, and assuming a constant temperature, as thevolume 30 of the internal gas increases, the pressure of the internalgas will decrease as will the air-spring effect. Conversely, as thevolume 30 of the internal gas decreases, the pressure of the internalgas will increase and so too will the stiffness of the air-spring. Withrespect to FIG. 3, the curve shown at 50 is a hypotheticalrepresentation of the output of a marine vibrator 5 at D meters depthwithout pressure compensation. The curve shown at 55 represents theoutput of the marine vibrator 5 at D+x meters depth with pressurecompensation. Pressure compensation may cause an increase in-internalgas pressure and thus a resulting increase in the air-spring effect. Asillustrated by FIG. 3, the resonance frequency of marine vibrator 5 mayshift higher with pressure compensation, thus showing how an increase inthe air-spring effect may result in a higher resonance frequency. Asillustrated, the increase in resonance frequency becomes more pronouncedat greater depths.

FIG. 4 illustrates simulated amplitude spectra from a finite elementsimulation showing the effect of the air-spring as a function of depth.The curves in FIG. 4 represent the output of a marine vibrator towed atvarying depth with pressure compensation. In particular, the curves inFIG. 4 represent the output of the marine vibrator towed at 0 meters, 50meters, 100 meters, and 120 meters, respectively, shown at 60, 65, 70,and 75. As illustrated, the increase in resonance frequency may be morepronounced at greater depths, thus indicating that the resonancefrequency increases as the air-spring is made stiffer.

In accordance with present embodiments, the spring constant of theair-spring may be adjusted by restricting gas flow in marine vibrator 5.By way of example, a variable gas flow restrictor 10 may be disposedwithin the marine vibrator internal volume, such that variable gas flowrestrictor 10 may change the volume of the internal gas 30, byrestricting flow of the internal gas throughout at least a portion ofthe volume of marine vibrator 5. This restriction in the flow may makethe air-spring more or less stiff. As the stiffness of the air-springimpacts the resonance frequency, the air-spring stiffness may beadjusted to thereby adjust the resonance frequency. This may beparticularly desirable if marine vibrator 5 is to be towed at differentdepths. In some embodiments, it may be desirable to have the resonancefrequency remain substantially constant (e.g., vary by no more than 5%)regardless of depth. However, as previously described, when marinevibrator 5 is towed at depth, the pressure of the internal gas may beincreased by the pressure-compensation system such that the air-springmay become stiffer as depth increases. For example, if marine vibrator 5has a resonance of 2.5 Hz at 120 meters, it may have a much lowerresonance (i.e. less than 2.5 Hz) at 50 meters. To compensate for thisstiffening of the air-spring, the gas flow in marine vibrator 5 may berestricted at shallower depths to make the air-spring stiffer, thusincreasing the resonance frequency to be more consistent with the higherresonance frequencies that occur with increasing depth.

With reference now to FIG. 5, an example embodiment of a variable gasflow restrictor 10 will now be described in more detail. As illustrated,variable gas flow restrictor 10 may have a sliding-plate structure thatcomprises a first plate 80 and a second plate 85. First plate 80 andsecond plate 85 may both comprise holes 90. First plate 80 and secondplate 85, as illustrated, may each be generally rectangular in shape insome embodiments; however, other plate configurations may be suitableincluding square, circular, elliptical, or irregular-shaped structures.The number of holes 90 in first plate 80 and second plate 85 may beselected in order to obtain the desired amount of gas flow. Each ofholes 90 may have a selected diameter and spacing based on the desiredamount of gas flow and desired resonance frequency, among others. Forexample, hole size may be reduced with increased spacing if less gasflow is desired while hole size may be increased with reduced spacing ifmore gas flow is desired. Holes 90 may, but need not be, of a consistentsize or shape within a single plate or relative from one plate to theother.

Variable gas flow restrictor 10 may be adjusted from (or to) a closed orpartially closed position (e.g., left side of FIG. 5) to (or from) anopen position (e.g., right side of FIG. 5). In the open position, holes90 in first plate 80 may be aligned with holes 90 in second plate 85such that openings 95 are formed in variable gas flow restrictor 10 andconsequently allowing the flow of the internal gas across openings 95.In the closed position, holes 90 in first plate 80 may be at leastpartially closed by second plate 85 thus restricting internal gas flowthrough openings 95. By movement of second plate 85, the size ofopenings 95 may be reduced, restricting gas flow. In other words, secondplate 85 may be positioned to effectively limit the size of openings 95.In some embodiments as shown on FIG. 5, second plate 85 may bepositioned to partially close variable gas flow restrictor 10 such thatholes 90 in first plate 80 are substantially blocked. An electric drive,pneumatic drive, hydraulic drive, or other suitable drive may be used toadjust openings 95 in variable gas flow restrictor 10. A linkage (notshown) may couple variable gas flow restrictor 10 to a control systemthat may operate to control the position of second plate 85 andconsequently the gas flow through openings 95. Variable gas flowrestrictor 10 may be actively or passively controlled, for example, tomaintain a substantially constant resonance frequency as the depth ofmarine vibrator 5 changes. For example, variable gas flow restrictor 10may be closed at shallower depths to restrict gas flow, thus stiffeningthe air-spring and increasing the frequency such that a constantresonance frequency is maintained as the depth of marine vibrator 5 isvaried. In some embodiments, variable gas flow restrictor 10 may bepassively adjusted, for example, based on a pressure sensor. In someembodiments, variable gas flow restrictor 10 may be remotely controlledfrom the tow vessel or a work boat (e.g., survey vessel 225 on FIG. 11).In some embodiments, variable gas flow restrictor 10 may be fixed inplace in some operations. It should be understood that first plate 80may be moveable in some embodiments while second plate 85 remainsstationary. Alternatively, second plate 85 may be moveable in someembodiments while first plate 80 remains stationary. As an alternativeto the use of a second plate 85, each of holes 90 in first plate 80 mayinstead be fitted with louvers or any other suitable covering (e.g.,flapper, guillotine device, etc.) that may be adjusted to permit orrestrict the flow of the marine vibrator internal gas through holes 90.Although FIG. 5 illustrates variable gas flow restrictor 10 as asliding-plate structure, other suitable mechanisms for restricting gasflow in marine vibrator 5 may be used in accordance with exampleembodiments, including hinged doors, roll-up doors, and the like. Forexample, a device (e.g., a plate, door, etc.) may be used to seal off aportion of the marine vibrator internal volume available to theair-spring.

Turning now to FIGS. 6-8, and with additional reference to FIG. 1,example embodiments of marine vibrator 5 will now be described. FIG. 6is a partial cross-sectional view of an example embodiment of marinevibrator 5. FIG. 7 is a cross-sectional view of the embodiment of marinevibrator 5 of FIG. 6 taken along line 1-1. FIG. 8 is a cross-sectionalview of the embodiment of marine vibrator 5 of FIG. 6 taken along line2-2.

In the illustrated embodiment, marine vibrator 5 includes a containmenthousing 100. Piston plates 15 may be flexibly coupled to containmenthousing 100, for example, by way of rubber seals 105. As best seen inFIGS. 6-8, piston plates 15 may each have mechanical spring elements 110attached to them. One or more drivers 20 may be disposed in containmenthousing 100 to cause the piston plates 15 to move back and forth. Thismotion of piston plates 15 may take advantage of the flexibility ofrubber seals 105. As would be understood by one of ordinary skill in theart with the benefit of this disclosure, rubber seals 105 do not need tobe made of rubber, but rather may be made from any material that allowsa flexible coupling of piston plates 15 to containment housing 100 asfurther discussed below.

Containment housing 100 may have first surface 115 and second surface120, which may be opposing one another. As best seen on FIGS. 6-8, firstopening 125 and second opening 130 may be formed respectively in thefirst surface 115 and the second surface 120. While not illustrated,some embodiments may include windows or openings 125, 130 that arelarger or smaller than piston plates 15. Marine vibrator 5 furthercomprises an interior volume 135 which may be at least partially definedby containment housing 100 and piston plates 15. In some embodiments,mechanical spring elements 110 and drivers 20 may be at least partiallydisposed within interior volume 135. In alternative embodiments,mechanical spring elements 110 and drivers 20 may be entirely disposedwithin interior volume 135. While not illustrated, in furtheralternative embodiments, mechanical spring elements 110 may be disposedoutside containment housing 100 so long as mechanical spring elements110 are coupled to fixture 25. In some embodiments, marine vibrator 5may be pressure compensated such that the pressure within interiorvolume 135 may be kept the same as the external pressure (i.e. thepressure on the side of piston plate 15 opposite that of interior volume135), thus enabling operation at greater depth, for example, up to about300 meters or more. Containment housing 100 together with piston plates15 and rubber seals 105 may form a waterproof housing for the othercomponents of marine vibrator 5, such as mechanical spring elements 110and drivers 20. Containment housing 100 may be constructed from anysuitable material, including, without limitation, steel (e.g., stainlesssteel), aluminum, a copper alloy, glass-fiber reinforced plastic (e.g.,glass-fiber reinforced epoxy), carbon fiber reinforced plastic, andcombinations thereof. Similarly, containment housing 100 as shown inFIGS. 6-8, may have the general shape of a rectangular box. It should beunderstood that other configurations of containment housing 100 may besuitable, including those having the general shape of a square box orother suitable shapes.

As illustrated, marine vibrator 5 comprises piston plates 15. Pistonplates 15 may typically be constructed of a material that will notdeform, bend or flex when in use. By way of example, piston plates 15may comprise, without limitation, steel (e.g., stainless steel),aluminum, a copper alloy, glass-fiber reinforced plastic (e.g.,glass-fiber reinforced epoxy), carbon fiber reinforced plastic, andcombinations thereof. In some embodiments, piston plates 15 may besubstantially flat and rectangular in shape. By way of example, pistonplate 15 shown on FIG. 1 is rectangular in shape. In some embodiments,piston plates 15 may have rounded or smooth corners. In someembodiments, piston plates 15 may in the form of flat, circular disks.By way of example, piston plates 15 may each be a flat, circular diskhaving substantially uniform thickness. However, other configurations,including both axially-symmetric and not, of piston plates 15 may besuitable for particular applications. By way of example, piston plates15 may be square, elliptical, or other suitable shape for providing thedesired acoustic energy. In alternative embodiments, piston plates 15may be curved, either convexly protruding into interior volume 135, orconcavely expanding interior volume 135. In general, piston plates 15have a thickness that provides stiffness and also withstands expectedpressures. As will be appreciated by those of ordinary skill in the artwith the benefit of this disclosure, the plate thickness may vary basedon the material of construction, among other factors. As will bediscussed in more detail below, the mass load of piston plates 15 andthe spring constant of mechanical spring elements 110 may be selected(i.e. tuned) in a manner to produce a first resonance frequency withinthe desired seismic frequency range when marine vibrator 5 is submergedin water at a depth of from about 0 meters to about 300 meters. While asingle piston plate 15 is illustrated on either side of fixture 25,embodiments may include more than one piston plate 15 on either side offixture 25. Moreover, embodiments may include piston plates 15 that aresmaller in size with respect to containment housing 100 as compared tothose illustrated on FIGS. 1 and 6-8.

With continued reference to FIGS. 1 and 6-8, piston plates 15 may eachbe secured to containment housing 100 in a manner that allows movementof piston plates 15 relative to containment housing 100 withsubstantially no bending or flexing of piston plates 15. In theembodiment of FIG. 1, a pair of piston plates 15 is shown. One of thepiston plates 15 may be disposed on one side of containment housing 100while the other piston plates 15 may be disposed on the opposing side ofcontainment housing 100. As illustrated, one of the piston plates 15 maybe coupled to the containment housing 100 at or near the first surface115 and the other piston plate 15 may be coupled to the containmenthousing 100 at or near the second surface 120. Piston plates 15 may eachcover a corresponding one of the first opening 125 or second opening 130in the respective first surface 115 and second surface 120 ofcontainment housing 100. In the illustrated embodiment, piston plates 15are coupled to containment housing 100 by way of rubber seals 105.Rubber seals 105 may not hold piston plates 15 in place but rather mayflex (or otherwise move) to permit movement of piston plates 15 at theirouter edges. In particular embodiments, piston plates 15 may function aspiston transducers, wherein each of the piston plates 15 moves backforth by actuation of the drivers 20. Movement of pistons plates 15 isillustrated in FIGS. 7 and 8 by arrows 136. In contrast toflextensional-shell type marine vibrators, piston plates 15 may not bendor flex in operation, but rather may move back and forth acting againstthe surrounding water.

Drivers 20 may be one of a variety of types of drivers 20, for exampleelectro-dynamic drivers. In some embodiments, the drivers 20 may be“moving coil” or “voice coil” drivers, which may provide the ability togenerate very large acoustic energy amplitudes. Although the particularembodiment described herein shows four uni-directional drivers utilizedin parallel, embodiments in which one or more bi-directional drivers,embodiments with one or more uni-directional drivers, or embodiments inwhich more or less than four uni-directional drivers are utilized, areeach within the scope of the invention. As best seen in FIGS. 7 and 8, apair of drivers 20 may be coupled to an interior surface 140 of onepiston plate 15, while another pair of drivers 20 may be coupled to aninterior surface 140 of the other piston plate 15. Drivers 20 may alsobe coupled to fixture 25.

As illustrated, drivers 20 may each comprise a uni-directional, movingcoil driver, comprising an electric coil 145, transmission element 150,and magnetic circuitry 155, which work together to generate a magneticfield. As illustrated, magnetic circuitry 155 may be connected tofixture 25, while transmission element 150 may connect to thecorresponding piston plate 15. In some embodiments (not illustrated),this arrangement may be reversed (i.e., magnetic circuitry 155 connectsto the corresponding piston plate 15, while transmission element 150connects to fixture 25). As illustrated, each transmission element 150may transfer the motion of the corresponding electric coil 145 tointerior surface 140 of the corresponding piston plate 15. Whenelectrical current I is applied to electric coil 145, a force F actingon electric coil 145 may be generated as follows:

F=IlB  (Eq. 1)

Where I is the current, l is the length of the conductor in electriccoil 145, and B is the magnetic flux generated by magnetic circuitry155. By varying the magnitude of the electrical current and consequentlythe magnitude of the force acting on electric coil 145, the length ofthe driver stroke may vary. Each driver 20 may provide stroke lengths ofseveral inches—up to and including about 10″—which may allow the marinevibrator 5 to generate enhanced amplitude acoustic energy output in thelow frequency ranges, for example, between about 1 Hz and about 100 Hz,and more particularly, between about 1 and 10 Hz when marine vibrator 5is submerged in water at a depth of from about 0 meters to about 300meters. Magnetic circuitry 155 may comprise permanent magnets, thoughany device capable of generating a magnetic flux may be incorporated.

In the illustrated embodiment, mechanical spring elements 110 (e.g., inthe form of coil springs) are disposed in containment housing 100 oneither side of fixture 25. As best seen in FIG. 6, pairs of mechanicalspring elements 110 may be located on either side of fixture 25, with afirst pair of mechanical spring elements 110 disposed on one side offixture 25, and a second pair of mechanical spring elements 110 may bedisposed on the opposing side of fixture 25. Mechanical spring elements110 in the first pair may be disposed on opposite sides of the drivers20 from one another, while the other pair of mechanical spring elements110 may also be disposed on opposite side of the drivers 20 from oneanother. Mechanical spring elements 110 may each extend between acorresponding one of piston plates 15 and fixture 25. Mechanical springelements 110 may be coupled to fixture 25 and at least one of pistonplates 15 to exert a biasing action against piston plates 15. A widevariety of different mechanical spring elements 110 may be used that aresuitable for exerting the desired biasing action against piston plates15, including both linear and non-linear springs. In particularembodiments, mechanical spring elements 110 may be any of a variety ofdifferent types of springs, including compression springs, torsionsprings, or other suitable springs for exerting the desired biasingaction. Specific examples of mechanical spring elements 110 that may beused include coil springs, flat springs, bow springs, and leaf springs,among others. Suitable mechanical spring elements 110 may be constructedfrom spring steel or other suitable resilient material, such asglass-fiber reinforced plastic (e.g., glass-fiber reinforced epoxy),carbon fiber reinforced plastic, and combinations thereof. In someembodiments, the dimensions, material make-up, and the shape ofmechanical spring elements 110 may be selected to provide a sufficientspring constant for vibrations in the seismic frequency range ofinterest when the marine vibrator 5 is submerged in water at a depth offrom about 0 meters to about 300 meters.

In the illustrated embodiment, marine vibrator 5 further includesvariable gas flow restrictor 10 disposed within interior volume 135 ofmarine vibrator 5. As illustrated, variable gas flow restrictor 10 maybe secured to fixture 25. As previously described, variable gas flowrestrictor 10 may be moveable between an open position and a closedposition to restrict gas flow in marine vibrator 5. By way of example,restriction of gas flow may be used to increase the first resonancefrequency by stiffening the air-spring.

In some embodiments, a fixture 25 suspends drivers 20 within containmenthousing 100. For example, in the illustrated embodiment, fixture 25extends along the major axis of containment housing 100 and may becoupled to either end of containment housing 100. Fixture 25 may becircular, square, rectangular, or other suitable cross-section asdesired for a particular application. An example of a suitable fixture25 may include a rod, beam, plate, or other suitable frame forsupporting internal components such as drivers 20 in containment housing100. In particular embodiments, fixture 25 should be fixed tocontainment housing 100 in a manner that restricts movement andtherefore prevents undesired contraction of the major axis ofcontainment housing 100. In particular embodiments, piston plates 15 maywork in symmetry above and below fixture 25. In other words, in someembodiments, fixture 25 may divide marine vibrator 5 into symmetricalhalves with respect to at least piston plates 15, mechanical springelements 110, and drivers 20.

In the illustrated embodiment, coupling of rubber seals 105 to pistonplates 15 is shown. Rubber seals 105 may also be coupled to containmenthousing 100, for example, to form a water-tight seal between pistonplates 15 and containment housing 100. In general, rubber seals 105 maybe configured to allow movement of piston plates 15 while alsomaintaining the appropriate seal. Rubber seals 105 may have significantcurvature to peimit significant amplitude of movement. By way ofexample, this permitted movement may further enable piston plates 15 tohave several inches of travel, e.g., piston plates 15 may move back andforth relative to containment housing 100 a distance of from about 1inch to about 10 inches (or more). Other techniques for permittingmovement may be used, including the use of seals with bellows oraccordion-type configurations.

As would be understood by one of ordinary skill in the art, the totalimpedance that may be experienced by a marine vibrator 5 may beexpressed as follows:

Z _(r) =R _(r) +jX _(r)  (Eq. 2)

where Z_(r) is total impedance, R_(r) is radiation impedance, and X_(r)is reactive impedance.

In an analysis of the energy transfer of marine vibrator 5, the systemmay be approximated as a baffled piston. In the expression of the totalimpedance that will be experienced, the radiation impedance R_(r) of abaffled piston may be:

R _(r) =πa ²ρ_(o) cR ₁(x)  (Eq. 3)

and the reactive impedance may be:

$\begin{matrix}{{X_{r} = {\pi \; a^{2}\rho_{o}{X_{1}(x)}}}{where}} & \left( {{Eq}.\mspace{14mu} 4} \right) \\{{x = {{2\; {ka}} = {\left( {4\pi \; {a/\lambda}} \right) = \left( {2\omega \; {a/c}} \right)}}}{{and}\mspace{14mu} {where}}} & \left( {{Eq}.\mspace{14mu} 5} \right) \\{{R_{1}(x)} = {1 - {\left( {2/x} \right)J_{1{(x)}}\mspace{14mu} {and}}}} & \left( {{Eq}.\mspace{14mu} 6} \right) \\{{X_{1}(x)} = {\left( \frac{4}{\pi} \right){\int_{0}^{\pi/2}{{\sin \left( {x\; \cos \; \alpha} \right)}\sin^{2}\alpha \ {\alpha}}}}} & \left( {{Eq}.\mspace{14mu} 7} \right)\end{matrix}$

where ρ_(o) is the density of water, ω=radial frequency, k=wave number,a=radius of piston, c=sound velocity, λ=wave length, and J₁=Besselfunction of the first order.

Using the Taylor series expansion on the above equations yields thefollowing:

$\begin{matrix}{{R_{1}(x)} = {\frac{x^{2}}{2^{2}{1!}{2!}} - \frac{x^{4}}{2^{4}{2!}{3!}} + \ldots}} & \left( {{Eq}.\mspace{14mu} 8} \right) \\{{X_{1}(x)} = {\frac{4}{\pi}\left( {\frac{x}{3} - \frac{x^{3}}{3^{2}5} + \frac{x^{5}}{3^{2}5^{2}7} - \ldots} \right.}} & \left( {{Eq}.\mspace{14mu} 9} \right)\end{matrix}$

For low frequencies, when x=2 ka is much smaller than 1, the real andimaginary part of the total impedance expression may be approximatedwith the first term of the Taylor expression. The expressions for lowfrequencies, when the wave length is much larger than the radius of thepiston becomes:

R ₁(x)=(½)(ka)²  (Eq. 10)

X ₁(x)→(8 ka)/(3 m)  (Eq. 11)

It follows that, for low frequencies, R will be a small number comparedto X, which suggests a very low efficiency signal generation. However,embodiments may introduce a resonance in the lower end of the frequencyspectrum so that low frequency acoustic energy may be generated moreefficiently. At resonance, the imaginary (reactive) part of theimpedance is cancelled, and marine vibrator 5 may be able to efficientlytransmit acoustic energy into the body of water.

FIG. 9 illustrates a cross-sectional view of one embodiment of marinevibrator 5 that comprises an alternative embodiment of mechanical springelements 110. This cross-sectional view is taken along line 3-3 of FIG.6. In contrast to the mechanical spring elements 110 of FIGS. 6-8 whichare illustrated as coiled springs, FIG. 9 illustrates mechanical springelements 110 in the form of a bow spring. In this cross-sectional viewof FIG. 9, certain elements of marine vibrator 5, such as the drivers20, are not visible.

The following description is for one of mechanical spring elements 110;however, because fixture 25 provides a line of symmetry, thisdescription is equally applicable to both of mechanical spring elements110. As illustrated in FIG. 9, one of mechanical spring elements 65 maybe coupled to one of piston plates 15 and fixture 25. Mechanical springelement 110 may be coupled to piston plate 10 at attachment point 160,which may be a fixed connection, for example, that does not permitmovement. Mechanical spring element 110 may be coupled to supplementalfixture 165, which may be in the form of a beam, rod, or other suitableframe for supporting mechanical spring element 110 in containmenthousing 100. Mechanical spring element 110 may be coupled tosupplemental fixture 165 by way of bearings 170. In particularembodiments, bearings 170 may be linear bearings that permit linearmovement of the ends of mechanical spring element 110 as represented byarrows 175. In this manner, mechanical spring element 110 may be allowedto flex and provide a biasing force to piston plate 15 upon itsmovement. Supplemental fixture 165 may be coupled to fixture 25 at oneor more of fixture attachment points 180, which may be fixed connectionsthat do not permit movement. Additionally, marine vibrator 5 of FIG. 9is illustrated with a variable gas flow restrictor 10 attached tofixture 25 in a substantially similar manner as was illustrated in FIGS.1 and 6-8. As in FIGS. 1 and 6-8, variable gas flow restrictor 10 may beused to vary the first resonance frequency by varying the gas flow andthus the stiffness of the air-spring. Therefore, the resonance frequencyfor marine vibrator 5 is selected based at least in part on variable gasflow restrictor 10.

Turning now to FIG. 10, marine vibrator 5 is illustrated as furthercomprising two mass spring elements 185 with weights 190 affixedthereto. Mass springs elements 185 shown on FIG. 10 may also be used inconjunction with the mechanical spring elements 110 shown on FIG. 9 (orother suitable type of mechanical spring element 110). As illustrated,mass spring elements 185 may be generally elliptically shaped. Asillustrated, mass spring elements 185 may be coupled to fixture 25 andpiston plates 15. In the illustrated embodiment, a pair of mass springelements 185 are shown on either side of fixture 25 so that marinevibrator 5 comprises four mass spring elements 185. However, it shouldbe understood that more or less than four mass spring elements 185 maybe utilized for a particular application. As will be described below, invarious embodiments, the spring constant of mass spring elements 185 andthe mass of weights 190 may be selected in a manner to achieve a secondsystem resonance frequency within the seismic frequency range ofinterest when marine vibrator 5 is submerged in water at a depth of fromabout 0 meters to about 300 meters. In a particular embodiment, marinevibrator 5 may exhibit a first resonance frequency of about 2.5 Hz and asecond resonance frequency of about 4.5 Hz when submerged in water at adepth of from about 0 meters to about 300 meters. Although a marinevibrator 5 that does not include mass spring elements 185, as shown inthe embodiment illustrated in FIGS. 6-8, may display a second resonancefrequency, the second resonance frequency would typically be much higherand thus outside the seismic frequency range of interest. Additionally,marine vibrator 5 of FIG. 10 is illustrated with a variable gas flowrestrictor 10 attached to fixture 25 in a substantially similar manneras was illustrated in FIGS. 1 and 6-8. As in FIGS. 1 and 6-8, variablegas flow restrictor 10 may be used to vary the first resonance frequencyby varying the gas flow and thus the stiffness of the air-spring.Therefore, the resonance frequency for marine vibrator 5 is selectedbased at least in part on variable gas flow restrictor 10.

In some embodiments, marine vibrator 5 may display at least oneresonance frequency (when submerged in water at a depth of from about 0meters to about 300 meters) between about 1 Hz to about 200 Hz. Inalternative embodiments, marine vibrator 5 may display at least oneresonance frequency (when submerged in water at a depth of from about 0meters to about 300 meters) between about 0.1 Hz and about 100 Hz,alternatively, between about 0.1 Hz and about 10 Hz, and alternatively,between about 0.1 Hz and about 5 Hz. In some embodiments, marinevibrator 5 may display at least two resonance frequencies of about 10 Hzor lower. In some embodiments, the first resonance frequency may beadjusted by restricting the gas flow in interior volume 135 of marinevibrator 5. In particular embodiments, the first resonance frequency maybe increased by the restriction of gas flow in marine vibrator 5. By wayof example, the first resonance frequency may be adjusted to besubstantially constant regardless of depth. In FIG. 10, the firstresonance frequency may result substantially from interaction of outerpiston plate 15 and mechanical spring element 110. The second resonancefrequency may result substantially from the interaction of mass springelements 185 with added weights 190.

In evaluating air-spring effects, finite element analysis may beutilized as known to those of ordinary skill in the art. In such ananalysis, the following principles may be relevant. Piston plate 15 ofmarine vibrator 5 is approximated as a baffled piston, then, for lowfrequencies, the mass load, or the equivalent fluid mass acting on thepiston plate may be:

M _(piston)=ρ_(o)(8a ³/3)  (Eq. 12)

where M_(plate) is the mass load acting on piston plate 15, ρ_(o) is thedensity of water surrounding marine vibrator 5, and a is the equivalentradius for a piston plate which corresponds to the size of piston plate15.

The stiffness of the entrained gas (air-spring) may be described by thefollowing general formula:

K _(variableairspring)=ΔVolume/Volume*P*γ  (Eq. 13)

where: K_(variableairspring) is the air-spring value, Volume is theinternal volume of marine vibrator 5, ΔVolume is the change in volumedue to the action of marine vibrator 5, P is the absolute pressure ofthe gas inside marine vibrator 5, and γ is the adiabatic constant whichis a unique property dependent on the chemical composition of the gas.

Therefore, when accounting for the air-spring effects, the firstresonance frequency, f_(resonance-1), due to interaction of piston plate15 and mechanical spring element 110 may be substantially determined bythe following mass spring relationship:

$\begin{matrix}{f_{{resonance}\text{-}1} = {\frac{1}{2\pi}\sqrt{\frac{K_{piston\_ spring} + K_{variableairspring}}{M_{piston}}}}} & \left( {{Eq}.\mspace{14mu} 14} \right)\end{matrix}$

where K_(piston) _(—) _(spring) is the spring constant of mechanicalspring elements 110, K_(variableairspring) is the gas-spring valuedetermined by the change in gas volume using, for example, Equation 13above, and M_(piston) is the mass load of piston plate 15. Accordingly,it may be possible, as shown above, to adjust the first resonancefrequency by compensating for the air-spring. By restriction of the gasflow, the effective volume of gas can be changed, which results in achange in the gas-spring value. The first resonance frequency shouldalso change as the air-spring value has also changed. For example, astiffer air-spring due to an increase in pressure or a reduction inbasic volume of gas will have a higher gas-spring value thus causing acorresponding increase in the first resonance frequency.

To achieve efficient energy transmission in the seismic frequency rangeof interest, it may be desirable to achieve a second resonance frequencywithin the seismic frequency range of interest. In the absence of massspring elements 185 (as shown in FIG. 10) with added weights 190 (alsoas shown in FIG. 10), the second resonance frequency would typicallyoccur when piston plate 10 has its second Eigen-mode. This resonancefrequency, however, is normally much higher than the first resonancefrequency and not desirable, and accordingly, would typically be outsidethe seismic frequency range of interest. As is evident from theforegoing equation, the resonance frequency will be reduced if mass loadon the piston plates 15 is increased. However, in order to addsufficient mass to achieve a second resonance frequency within theseismic frequency range of interest, the amount of mass required toachieve a desirable second resonance frequency may make such a systemless practical for use in marine seismic surveying operations.

Therefore, in some embodiments, mass spring elements 185 may be includedinside marine vibrator 5 with added weights 190 on the side of massspring elements 185. Mass spring elements 185 may have a transformationfactor T_(spring) between the long and short axis of its ellipse, sothat the deflection of the two side portions will have a higheramplitude than the deflection of the end attached to piston plates 15and drivers 20.

The effect of such added weights 190 is equivalent to adding mass on theend of driver 20 where it is coupled to piston plate 15.

M _(spring)=(T _(spring))² ·M _(added)  (Eq. 14)

Use of mass spring elements 185 with added weights 190, may allow thesecond resonance frequency of the system to be tuned so that the secondresonance frequency is within the seismic frequency range of interest,thereby improving the efficiency of marine vibrator 5 in the seismicfrequency range of interest.

$\begin{matrix}{f_{{resonance}\; 2} = {\frac{1}{2\pi}\sqrt{\frac{K_{spring} + K_{piston\_ spring}}{{\left( T_{spring} \right)^{2} \cdot M_{added}} + M_{piston} + M_{{mass}\mspace{14mu} {load}}}}}} & \left( {{Eq}.\mspace{14mu} 15} \right)\end{matrix}$

where K_(spring) is the spring constant of mass spring elements 185, andK_(piston) _(—) _(spring) is the spring constant of mechanical springelements 110 attached to piston plate 15.

Accordingly, it may be possible, as shown above, to select weights 190on mass spring elements 185 to tune the second resonance frequency. Itmay also be possible to select the extent of influence the secondresonance frequency may have on the system. By way of example, if massspring elements 185 have low spring constants compared to mechanicalspring element 110 coupled to piston plate 15, and a matching weight 190is added to mass spring elements 185, mass spring elements 185 withweights 190 will function relatively independently from mechanicalspring element 110 attached to piston plate 15. In such cases, thesecond resonance frequency may be as follows:

$\begin{matrix}{f_{{resonance}\; 2} = {\frac{1}{2\pi}\sqrt{\frac{K_{spring}}{\left( T_{spring} \right)^{2} \cdot M_{added}}}}} & \left( {{Eq}.\mspace{14mu} 16} \right)\end{matrix}$

In the same way, it may also be possible in some embodiments to make thesecond resonance frequency very large by selecting a high springconstant for mass spring elements 185 with a matching weight 190 suchthat the second resonance frequency will have a larger amplitude thanthe first resonance frequency.

FIG. 11 illustrates an example technique for acquiring geophysical datathat may be used with embodiments of the present techniques. In theillustrated embodiment, a survey vessel 225 moves along the surface of abody of water 230, such as a lake or ocean. The survey vessel 225 mayinclude thereon equipment, shown generally at 235 and collectivelyreferred to herein as a “recording system.” The recording system 235 mayinclude devices (none shown separately) for detecting and making a timeindexed record of signals generated by each of seismic sensors 240(explained further below) and for actuating a marine vibrator 5 atselected times. The recording system 235 may also include devices (noneshown separately) for determining the geodetic position of the surveyvessel 225 and the various seismic sensors 240.

As illustrated, survey vessel 225 (or a different vessel) may tow marinevibrator 5 in body of water 230. Source cable 245 may couple marinevibrator 5 to survey vessel 225. Marine vibrator 5 may be towed in bodyof water 230 at a depth ranging from 0 meters to about 300 meters, forexample. While only a single marine vibrator 5 is shown in FIG. 11, itis contemplated that embodiments may include more than one marinevibrator 5 (or other type of sound source) towed by survey vessel 225 ora different vessel. In some embodiments, one or more arrays of marinevibrators 5 may be used. At selected times, marine vibrator 5 may betriggered, for example, by recording system 235, to generate acousticenergy. Survey vessel 225 (or a different vessel) may further tow atleast one sensor streamer 250 to detect the acoustic energy thatoriginated from marine vibrator 5 after it has interacted, for example,with rock formations 255 below water bottom 260. As illustrated, bothmarine vibrator 5 and sensor streamer 250 may be towed above waterbottom 260. Sensor streamer 250 may contain seismic sensors 240 thereonat spaced apart locations. In some embodiments, more than one sensorstreamer 250 may be towed by survey vessel 225, which may be spacedapart laterally, vertically, or both laterally and vertically. While notshown, some marine seismic surveys locate the seismic sensors 240 onocean bottom cables or nodes in addition to, or instead of, a sensorstreamer 250. Seismic sensors 240 may be any type of seismic sensorsknown in the art, including hydrophones, geophones, particle velocitysensors, particle displacement sensors, particle acceleration sensors,or pressure gradient sensors, for example. By way of example, seismicsensors 240 may generate response signals, such as electrical or opticalsignals, in response to detected acoustic energy. Signals generated byseismic sensors 240 may be communicated to recording system 235. Thedetected energy may be used to infer certain properties of thesubsurface rock, such as structure, mineral composition and fluidcontent, thereby providing information useful in the recovery ofhydrocarbons.

In accordance with an embodiment of the invention, a geophysical dataproduct may be produced. The geophysical data product may includegeophysical data that is obtained by a process that includes detectingthe acoustic energy originating from marine vibrator 5. The geophysicaldata product may be stored on a non-transitory, tangiblecomputer-readable medium. The geophysical data product may be producedoffshore (i.e. by equipment on a vessel) or onshore (i.e. at a facilityon land) either within the United States or in another country. If thegeophysical data product is produced offshore or in another country, itmay be imported onshore to a facility in the United States. Once onshorein the United States, geophysical analysis, including further dataprocessing, may be performed on the data product.

The foregoing figures and discussion are not intended to include allfeatures of the present techniques to accommodate a buyer or seller, orto describe the system, nor is such figures and discussion limiting butexemplary and in the spirit of the present techniques.

What is claimed is:
 1. A marine vibrator comprising: a containmenthousing; a piston plate; a fixture coupled to the containment housing; amechanical spring element coupled to the piston plate and to thefixture; a driver coupled to the piston plate and to the fixture; and avariable gas flow restrictor disposed in an interior volume of themarine vibrator, wherein the marine vibrator has a resonance frequencyselectable based at least in part on the variable gas flow restrictor.2. The marine vibrator of claim 1, wherein the marine vibrator has atleast one resonance frequency of about 10 Hz or lower when submerged inwater at a depth of from about 0 meters to about 300 meters.
 3. Themarine vibrator of claim 1, wherein the driver is a moving coil driveror a linear servo motor.
 4. The marine vibrator of claim 1, comprisinganother variable gas flow restrictor disposed in the interior volume ofthe marine vibrator.
 5. The marine vibrator of claim 1, wherein thevariable gas flow restrictor comprises a first plate and a second plate,wherein the first plate comprises holes and the second plate comprisesholes, and wherein either the first plate or the second plate ismoveable to at least partially cover the holes in the other plate. 6.The marine vibrator of claim 1, wherein the gas flow restrictorcomprises a sliding-plate structure.
 7. The marine vibrator of claim 1,wherein the variable gas flow restrictor is remotely controlled.
 8. Themarine vibrator of claim 1, wherein the mechanical spring elementcomprises at least one type of spring selected from the group consistingof: a bow spring, a coil spring, a flat spring, and a leaf spring. 9.The marine vibrator of claim 1, further comprising a second mechanicalspring element disposed on an opposite side of the driver from themechanical spring element.
 10. The marine vibrator of claim 1, whereinthe piston plate is coupled to the containment housing by way of arubber seal, the piston plate covering an opening in a first surface ofthe containment housing.
 11. The marine vibrator of claim 1, wherein themarine vibrator further comprises a mass spring element having weightsaffixed thereto, the mass spring element being coupled between thefixture and the piston plate.
 12. A method comprising: towing a marinevibrator in a body of water in conjunction with a marine seismic survey;and triggering the marine vibrator to cause one or more piston plates inthe marine vibrator to move back and forth wherein one or moremechanical spring elements exert a biasing force against the one or morepiston plates, the one or more mechanical spring elements being coupledto the one or more piston plates and a fixture in the marine vibrator;and varying the gas flow in an internal volume of the marine vibrator.13. The method of claim 12, wherein the marine vibrator is towed at afirst depth of from about 0 meters to about 300 meters, wherein themethod further comprises towing the acoustic vibrator at a second depth,and wherein the gas flow is restricted in the marine vibrator when towedat the first depth such that a first resonance frequency of the acousticvibrator is substantially constant when towing depth varies from thefirst depth to the second depth.
 14. The method of claim 12, wherein thevarying the gas flow comprises restricting the flow of gas through avariable gas flow restrictor by limiting the size of one or moreopenings in the variable gas flow restrictor.
 15. The method of claim14, wherein the varying the gas flow further comprises moving a plate toat least partially obstruct the one or more openings in the variable gasflow restrictor.
 16. The method of claim 12, further comprising loweringthe marine vibrator in the body of water, and opening a variable gasflow restrictor to allow increased gas flow in the marine vibrator asthe marine vibrator is lowered in the body of water.
 17. The method ofclaim 12, wherein the marine vibrator generates a first resonancefrequency within a frequency range of about 1 Hz and about 10 Hz. 18.The method of claim 12, further comprising: obtaining geophysical data;and processing the geophysical data to generate a geophysical dataproduct, wherein the geophysical data product is obtained by a processthat includes detecting acoustic energy originating from the marinevibrator.
 19. The method of claim 18, further comprising recording thegeophysical data product on a tangible, non-volatile computer-readablemedium suitable for importing onshore.
 20. The method of claim 19,further comprising performing geophysical analysis onshore on thegeophysical data product.